FIELD: power, transport and chemical mechanical engineering, possible use in gas-turbine plants.
SUBSTANCE: in accordance to fuel combustion method, fuel stream is separated at least onto three jets, which are fed successively in different cross-sections into air flow, after that fuel and air are mixed in different cross-sections to create a "weak" homogeneous fuel-air mixture, which is then fed into half-limited space filled with hot combustion products, where aforementioned mixture burns with creation of combustion products and emission of heat. Fuel jets are fed into air flow in such a way that a certain relation is maintained between characteristic times. Burner for realizing fuel combustion method contains external cylindrical manacle ring, blade air swirler coaxial with aforementioned manacle ring, circular pre-chamber, at intake of which fuel-dispensing device is provided.
EFFECT: increased stability of burning process.
4 dwg
Title | Year | Author | Number |
---|---|---|---|
HEATER | 2007 |
|
RU2348864C2 |
BURNER | 1996 |
|
RU2099639C1 |
BURNER | 2007 |
|
RU2343352C1 |
COMBUSTION CHAMBER | 1993 |
|
RU2087805C1 |
METHOD OF BURNING FUEL | 2001 |
|
RU2213296C2 |
FORECHAMBER OF COMBUSTION CHAMBER | 1994 |
|
RU2086857C1 |
METHOD OF BURNING FUEL | 1998 |
|
RU2128807C1 |
METHOD OF CONTROL OF FUEL DELIVERY TO COMBUSTION CHAMBER AND COMBUSTION CHAMBER FOR REALIZATION OF THIS METHOD | 1993 |
|
RU2083928C1 |
COMBUSTION CHAMBER | 1994 |
|
RU2086856C1 |
COMBUSTION CHAMBER PREMIXING CAVITY | 1993 |
|
RU2083926C1 |
Authors
Dates
2007-06-10—Published
2006-04-04—Filed